Testing the gravitational redshift during VERITAS cruise phase

dc.contributor.authorMarchi, Fabrizio De
dc.contributor.authorCascioli, Gael
dc.contributor.authorEly, Todd
dc.contributor.authorIess, Luciano
dc.contributor.authorBurt, Eric A.
dc.contributor.authorHensley, Scott
dc.contributor.authorMazarico, Erwan
dc.date.accessioned2022-12-20T20:23:12Z
dc.date.available2022-12-20T20:23:12Z
dc.date.issued2022-11-16
dc.description.abstractThe NASA Discovery-class mission VERITAS, selected in June 2021, will be launched towards Venus in 2027. In addition to the science instrumentation that will build global foundational geophysical datasets, VERITAS proposed to conduct a technology demonstration for the Deep Space Atomic Clock (DSAC-2). A first DSAC successfully operated in low-Earth orbit for more than two years, demonstrated the trapped ion atomic clock technology, and established a new level of performance for clocks in space. DSAC-2 would have further improvements in size, power, and performance. It would host a 1×10-¹³ grade USO to produce a frequency output with short-term stability of less than 2×10-¹³/√T (where τ is the averaging time). In this work, we investigate the possibility of leveraging DSAC-2's frequency stability to measure possible discrepancies in the redshift predicted by General Relativity. With its capability of establishing a one-way downlink Doppler link with Earth stations, DSAC-2 would enable precise tests of the dependency of the redshift on the location and velocity of the spacecraft and the Earth, thus providing improved tests of the Local Lorentz Invariance and Local Position Invariance. We perform accurate simulations of the experiment that would take place during the VERITAS cruise phase. We consider different parametrizations of the possible violations of the General Relativity, different operational conditions, and a wide spectrum of expected measurement performance assumptions. We show that DSAC-2 onboard VERITAS would provide new and improved constraints with respect to the current knowledge.en_US
dc.description.sponsorshipFDM, GC and LI acknowledge support from the Italian Space agency under contracts 2020-15-HH.0 and 2022-15-HH.0. A portion of the work described in this paper was carried out at the Jet Propulsion Laboratory, California Institute of Technology, under a contract with the National Aeronautics and Space Administration (80NM0018D0004). The authors are thankful to S. Smrekar for useful discussions. FDM would like to thank N. Bartel for the fruitful discussion at the COSPAR 2022 Assembly.en_US
dc.description.urihttps://arxiv.org/abs/2211.08964en_US
dc.format.extent12 pagesen_US
dc.genrejournal articlesen_US
dc.genrepreprintsen_US
dc.identifierdoi:10.13016/m2osug-r0de
dc.identifier.urihttps://doi.org/10.48550/arXiv.2211.08964
dc.identifier.urihttp://hdl.handle.net/11603/26481
dc.language.isoen_USen_US
dc.relation.isAvailableAtThe University of Maryland, Baltimore County (UMBC)
dc.relation.ispartofUMBC Center for Space Sciences and Technology
dc.relation.ispartofUMBC Faculty Collection
dc.rightsThis work was written as part of one of the author's official duties as an Employee of the United States Government and is therefore a work of the United States Government. In accordance with 17 U.S.C. 105, no copyright protection is available for such works under U.S. Law.en_US
dc.rightsPublic Domain Mark 1.0*
dc.rights.urihttp://creativecommons.org/publicdomain/mark/1.0/*
dc.titleTesting the gravitational redshift during VERITAS cruise phaseen_US
dc.typeTexten_US
dcterms.creatorhttps://orcid.org/0000-0001-9070-7947en_US

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